FR2927686B1 - Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef. - Google Patents

Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef.

Info

Publication number
FR2927686B1
FR2927686B1 FR0851087A FR0851087A FR2927686B1 FR 2927686 B1 FR2927686 B1 FR 2927686B1 FR 0851087 A FR0851087 A FR 0851087A FR 0851087 A FR0851087 A FR 0851087A FR 2927686 B1 FR2927686 B1 FR 2927686B1
Authority
FR
France
Prior art keywords
raidi
swivel
composite panel
aircraft part
panel self
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR0851087A
Other languages
English (en)
Other versions
FR2927686A1 (fr
Inventor
Philippe Vallee
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
EADS SOCATA
Original Assignee
EADS SOCATA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR0851087A priority Critical patent/FR2927686B1/fr
Application filed by EADS SOCATA filed Critical EADS SOCATA
Priority to EP09720526.4A priority patent/EP2242683B1/fr
Priority to ES09720526.4T priority patent/ES2583555T3/es
Priority to US12/866,751 priority patent/US20100320331A1/en
Priority to CA2714433A priority patent/CA2714433C/fr
Priority to JP2010547229A priority patent/JP2011512298A/ja
Priority to PCT/FR2009/050270 priority patent/WO2009112735A1/fr
Priority to BRPI0908084-8A priority patent/BRPI0908084A2/pt
Publication of FR2927686A1 publication Critical patent/FR2927686A1/fr
Application granted granted Critical
Publication of FR2927686B1 publication Critical patent/FR2927686B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/16—Fairings movable in conjunction with undercarriage elements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/23—Sheet including cover or casing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Moulding By Coating Moulds (AREA)
  • Superstructure Of Vehicle (AREA)
  • Securing Of Glass Panes Or The Like (AREA)
FR0851087A 2008-02-20 2008-02-20 Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef. Expired - Fee Related FR2927686B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0851087A FR2927686B1 (fr) 2008-02-20 2008-02-20 Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef.
ES09720526.4T ES2583555T3 (es) 2008-02-20 2009-02-19 Panel pivotante compuesto, rigidizado y monolítico, en particular para una parte móvil de una aeronave
US12/866,751 US20100320331A1 (en) 2008-02-20 2009-02-19 Unitary, Self-Stiffened and Pivoting Composite Panel, in Particular for a Mobile Part of an Aircraft
CA2714433A CA2714433C (fr) 2008-02-20 2009-02-19 Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef
EP09720526.4A EP2242683B1 (fr) 2008-02-20 2009-02-19 Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef
JP2010547229A JP2011512298A (ja) 2008-02-20 2009-02-19 特に航空機の移動部分のための、統一された、自己補強された、かつ、旋回式の複合パネル
PCT/FR2009/050270 WO2009112735A1 (fr) 2008-02-20 2009-02-19 Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef
BRPI0908084-8A BRPI0908084A2 (pt) 2008-02-20 2009-02-19 Painel compósito monolítico autoreforçado e articulado, principalmente para uma parte móvel de uma aeronave

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0851087A FR2927686B1 (fr) 2008-02-20 2008-02-20 Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef.

Publications (2)

Publication Number Publication Date
FR2927686A1 FR2927686A1 (fr) 2009-08-21
FR2927686B1 true FR2927686B1 (fr) 2010-10-08

Family

ID=39855738

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0851087A Expired - Fee Related FR2927686B1 (fr) 2008-02-20 2008-02-20 Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef.

Country Status (8)

Country Link
US (1) US20100320331A1 (fr)
EP (1) EP2242683B1 (fr)
JP (1) JP2011512298A (fr)
BR (1) BRPI0908084A2 (fr)
CA (1) CA2714433C (fr)
ES (1) ES2583555T3 (fr)
FR (1) FR2927686B1 (fr)
WO (1) WO2009112735A1 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5134258B2 (ja) 2007-02-09 2013-01-30 ユニ・チャーム株式会社 動物用トイレ砂
US8703268B2 (en) * 2009-11-13 2014-04-22 The Boeing Company Morphing panel structure
CN102501966B (zh) * 2011-11-07 2016-04-13 中国商用飞机有限责任公司 一种用于飞机舱门的扰流片及装有该扰流片的飞机舱门
EP2599711B1 (fr) * 2011-12-01 2017-07-26 Airbus Operations S.L. Cadre fortement chargé d'un fuselage d'avion doté d'un réseau structuré de treillis
EP2876044B1 (fr) 2013-11-21 2018-09-12 Airbus Operations GmbH Composant de coin de porte passager et procédé de fabrication d'un tel composant d'aéronef ou d'engin spatial
EP3536602B1 (fr) * 2014-10-16 2021-09-15 Airbus Operations GmbH Structure de panneau et procédé associé
US10724258B2 (en) * 2015-05-05 2020-07-28 West Virginia University Durable, fire resistant, energy absorbing and cost-effective strengthening systems for structural joints and members
EP3173331B1 (fr) 2015-11-30 2019-04-24 Airbus Operations GmbH Panneau de couverture pour un composant structurel
US20180099736A1 (en) * 2016-10-12 2018-04-12 The Boeing Company Aircraft wings, aircraft, and related methods
EP3601037B1 (fr) * 2017-03-30 2023-08-02 C&D Zodiac, Inc. Ensemble panneau de paroi latérale
CN108194817A (zh) * 2018-01-18 2018-06-22 安徽道智能制造技术有限公司 一种汽车专用宽板线框型面板结构
CN111140763A (zh) * 2018-11-02 2020-05-12 彭志军 一种带加强筋与锁扣结构的复合型板材
FR3107254A1 (fr) * 2020-02-18 2021-08-20 Airbus Operations (S.A.S.) Procédé de fabrication d’une structure aérodynamique mobile d’aéronef et structure aérodynamique mobile d’aéronef ainsi obtenue

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451131A (en) * 1940-09-06 1948-10-12 Vidal Corp Method of making reinforced structures
US3300354A (en) * 1962-04-18 1967-01-24 Whittaker Corp Method of making a filament wound sandwich core
US5262220A (en) * 1991-06-18 1993-11-16 Chem-Tronics, Inc. High strength structure assembly and method of making the same
ATE284346T1 (de) * 2001-01-26 2004-12-15 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
DE102005057907B4 (de) * 2005-12-02 2012-03-22 Eurocopter Deutschland Gmbh Luftfahrzeug-Druckkabinentür aus Faserverbundwerkstoff

Also Published As

Publication number Publication date
CA2714433A1 (fr) 2009-09-17
US20100320331A1 (en) 2010-12-23
BRPI0908084A2 (pt) 2015-08-25
ES2583555T3 (es) 2016-09-21
FR2927686A1 (fr) 2009-08-21
EP2242683B1 (fr) 2016-04-20
CA2714433C (fr) 2016-09-27
EP2242683A1 (fr) 2010-10-27
WO2009112735A1 (fr) 2009-09-17
JP2011512298A (ja) 2011-04-21

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